Viscous Interaction Phenomena in Supersonic and Hypersonic Flow.

Abstract

The symposium focused on departures from the classical boundary layer theories toward shock wave-boundary layer interactions with their attendant flow separation and reattachment and toward the three-dimensional viscous interactions of practical configurations. It thus dealt with one of the key problem areas associated with high speed supersonic aircraft, lifting-reentry vehicles, and potential hypersonic cruise vehicles. Such configurations are highly three-dimensional with complex flows involving strong viscous-inviscid interactions in regions of compression such as in air breathing engine inlets, at wing-body junctions, and over control surfaces. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1970
Accession Number
AD0714362

Entities

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerospace Craft
  • Air Breathing
  • Air Breathing Engines
  • Aircrafts
  • Boundaries
  • Boundary Layer
  • Control Surfaces
  • Flow
  • Flow Separation
  • Hypersonic Flow
  • Lifting Reentry Vehicles
  • Reentry Vehicles
  • Shock Waves
  • Supersonic Aircraft
  • Three Dimensional
  • Vehicles

Fields of Study

  • Physics

Readers

  • Academic Conference Management
  • Aerospace Engineering
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow